US2038639A - Method of producing castings - Google Patents
Method of producing castings Download PDFInfo
- Publication number
- US2038639A US2038639A US682275A US68227533A US2038639A US 2038639 A US2038639 A US 2038639A US 682275 A US682275 A US 682275A US 68227533 A US68227533 A US 68227533A US 2038639 A US2038639 A US 2038639A
- Authority
- US
- United States
- Prior art keywords
- casting
- silicon
- castings
- chromium
- melt
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000005266 casting Methods 0.000 title description 35
- 238000000034 method Methods 0.000 title description 5
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 21
- 229910052710 silicon Inorganic materials 0.000 description 21
- 239000010703 silicon Substances 0.000 description 21
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 14
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 9
- 229910052804 chromium Inorganic materials 0.000 description 9
- 239000011651 chromium Substances 0.000 description 9
- 239000000155 melt Substances 0.000 description 9
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 7
- 239000003795 chemical substances by application Substances 0.000 description 7
- 229910052742 iron Inorganic materials 0.000 description 7
- 239000000203 mixture Substances 0.000 description 7
- 229910052799 carbon Inorganic materials 0.000 description 6
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 4
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 4
- 229910052698 phosphorus Inorganic materials 0.000 description 4
- 239000011574 phosphorus Substances 0.000 description 4
- 229910052717 sulfur Inorganic materials 0.000 description 4
- 239000011593 sulfur Substances 0.000 description 4
- 229910001018 Cast iron Inorganic materials 0.000 description 3
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 3
- 238000004458 analytical method Methods 0.000 description 3
- 229910001021 Ferroalloy Inorganic materials 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 229910000676 Si alloy Inorganic materials 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 101100072702 Drosophila melanogaster defl gene Proteins 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 235000000396 iron Nutrition 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C37/00—Cast-iron alloys
- C22C37/06—Cast-iron alloys containing chromium
Definitions
- the present invention is based on the discovery that the hardening effect of carbide forming elements is decreased, and the strength, ductility, and machinability of the casting are improved, if a substantial amount of a graphitizing agent,
- the final composition of the 5 casting should be substantially 1% to 4% carbon, 1% to 4% graphitizing agents, 0.15% to 1% manganese, up to about 0.5% sulfur, 0.05% to 0.3% phosphorus, 0.1% to 35% carbide forming elements, remainder iron.
- the greatest use of the invention may be in producing castings containing 0.1% to 2% chromium as the carbide forming element; .but the improvement in properties is found to be marked in castings containing up to 35% and more chromium or other carbide forming element.
- the invention provides castings havconium, is added to the molten iron shortly before ing a, transverse test strength greater than about the melt is cast rather than during the initial 4500 pounds, as compared to 3000-4000 pounds melting period.
- the graphitizing agent is prefin iron castings previously known. erably added in the ladle.
- castings 4 and 5 chinability results, as compared to a casting havwere substantially identical.
- the silicon in cast- 40 ing the same composition but treated with the ings numbers 1, 2 and 4 was added in the furnace graphitizing agent, at a time other than shortly in the usual manner; while part of the silicon before pouring.
- the treatment also results in a in castings numbers 3 and 5 was added in the marked refinement of the structure of the castladle.
- Casting number 3 was materially stronger, ing, and serves to break up or to inhibit the more ductile, and more easily machinable than formation of large crystallites of carbides, which casting number 2, and stronger, harder, and more doubtless contributes to the improved machinawear resistant than casting number 1.
- the best. casting number 5 was materially stronger and results are obtained when the amount of silicon more easily machinable than casting number 4, and other grap t agents present during the
- the graphitizing agent may be added as a meltin p r d s relatively low so t a a large metal or a ferroalloy.
- the carbide forming agent proportion of the total final silicon may be dded may be added in the furnace or in the ladle, as immediate y before casting a metal, ferroalloy, or compound.
- the ing the content of carbide forming element in addition may, conveniently be made as a siliconchromium alloy, or as a ferrochromium-silicon alloy, or as a low melting copper, chromium, silicon alloy.
- Method of producing a ferrous alloy casting having substantially the composition: 0.1% to chromium, 1% to 4% silicon, 1% to 4% carbon, 0.15% to 1% manganese, up to about 0.5% sulfur, up to about 0.3% phosphorus, the remainder iron, and characterized by improved machinability, ductility, and strength, which comprises forming a melt the silicon content of which is materially less than is desired in the casting, adding silicon, and casting the melt substantially immediately after the addition of silicon.
- Method of producing a ferrous alloy casting having substantially the composition: 0.1% to 15% chromium, 1% to 4% silicon, 1% to 4% carbon, 0.15% to 1% manganese, up to about 0.5% sulfur, up to about 0.3% phosphorus, the remainder iron, and characterized by improved machinability, ductility, and strength, which comprises forming a melt the silicon content of which is materially less than is desired in the casting, add-- ing silicon, and casting the melt substantially immediately after the addition of silicon.
- Method of producing a ferrous alloy casting having substantially the composition: 0.1% to 2% chromium, 1% to 4% silicon, 1% to 4% carbon, 0.15% to 1% manganese, upto about 0.5% sulfur, up to about 0.3% phosphorus, the remainder iron, and characterized by improved machinability, ductility, and strength, which comprises forming a melt the silicon content of which is materially less than is desired in the casting, adding silicon, and casting the melt substantially immediately after the addition of silicon.
- Method of producing an alloyed cast-iron casting containing from 0.1% to 15% chromium which comprises forming a melt of chromiumalloyed iron the silicon content of which is materially less than is desired in the casting, adding silicon, and casting the melt substantially immediately after the addition of silicon, whereby is produced a casting having a structure consisting chiefly of a pearlitic ground mass, small graphite flakes, and small widely dispersed non-dendritic carbide particles distributed substantially uniformly throughout the ground mass the proportion of carbide present being only a minor fraction of that normally present in cast iron of similar composition.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
Description
Patented Apr. 28, 1936 UNITED STATES PATENT OFFICE mesne assignments,
to Union Carbide and Carbon Corporation, a corporation of New York No Drawing. Application July 26, 1933,
' Serial No. 682,275
4 Claims.
The present invention is based on the discovery that the hardening effect of carbide forming elements is decreased, and the strength, ductility, and machinability of the casting are improved, if a substantial amount of a graphitizing agent,
any given casting composition without decreasing or destroying machinability.
All cast irons containing more than about 1% carbon may be benefited by the use of the invention. In general, the final composition of the 5 casting should be substantially 1% to 4% carbon, 1% to 4% graphitizing agents, 0.15% to 1% manganese, up to about 0.5% sulfur, 0.05% to 0.3% phosphorus, 0.1% to 35% carbide forming elements, remainder iron. The greatest use of the invention may be in producing castings containing 0.1% to 2% chromium as the carbide forming element; .but the improvement in properties is found to be marked in castings containing up to 35% and more chromium or other carbide forming element.
The table given below is illustrative of the improvement in the properties of cast iron attainable according to the invention:
Analysis of casting Transverse tests Tensile Hardness Casting number Ladle addition strength, Briuell 950; %Bi 3 53 Defl. m. Pmmds Nil 2. 52 3,050 0.093 31,400 170 1.01 2. 3,100 0.000 41,050 310 1.00 2. 42 5,025 0.153 00,550 200 14.04 2. 52 3,000 0,01 14.59 an 4,000 0.085
for example, silicon, nickel, aluminum, or zir- Ingeneral, the invention provides castings havconium, is added to the molten iron shortly before ing a, transverse test strength greater than about the melt is cast rather than during the initial 4500 pounds, as compared to 3000-4000 pounds melting period. The graphitizing agent is prefin iron castings previously known. erably added in the ladle. The analyses of castings 1, 2, and 3, respec- When a graphitizing element is added in th tively, were substantially identical with the exabove described manner shortly before pouring, ceptionof the chromium content of casting num-' a marked increase in strength, ductility, and maher 1. Likewise, the analyses of castings 4 and 5 chinability results, as compared to a casting havwere substantially identical. The silicon in cast- 40 ing the same composition but treated with the ings numbers 1, 2 and 4 was added in the furnace graphitizing agent, at a time other than shortly in the usual manner; while part of the silicon before pouring. The treatment also results in a in castings numbers 3 and 5 was added in the marked refinement of the structure of the castladle. Casting number 3 was materially stronger, ing, and serves to break up or to inhibit the more ductile, and more easily machinable than formation of large crystallites of carbides, which casting number 2, and stronger, harder, and more doubtless contributes to the improved machinawear resistant than casting number 1. Similarly, bility and strength of the castings. The best. casting number 5 was materially stronger and results are obtained when the amount of silicon more easily machinable than casting number 4, and other grap t agents present during the The graphitizing agent may be added as a meltin p r d s relatively low so t a a large metal or a ferroalloy. The carbide forming agent proportion of the total final silicon may be dded may be added in the furnace or in the ladle, as immediate y before casting a metal, ferroalloy, or compound. If chromium The invention thus affords a means of increasand silicon are both' to be added in the ladle, the ing the content of carbide forming element in addition may, conveniently be made as a siliconchromium alloy, or as a ferrochromium-silicon alloy, or as a low melting copper, chromium, silicon alloy.
I claim:
1. Method of producing a ferrous alloy casting having substantially the composition: 0.1% to chromium, 1% to 4% silicon, 1% to 4% carbon, 0.15% to 1% manganese, up to about 0.5% sulfur, up to about 0.3% phosphorus, the remainder iron, and characterized by improved machinability, ductility, and strength, which comprises forming a melt the silicon content of which is materially less than is desired in the casting, adding silicon, and casting the melt substantially immediately after the addition of silicon.
2. Method of producing a ferrous alloy casting having substantially the composition: 0.1% to 15% chromium, 1% to 4% silicon, 1% to 4% carbon, 0.15% to 1% manganese, up to about 0.5% sulfur, up to about 0.3% phosphorus, the remainder iron, and characterized by improved machinability, ductility, and strength, which comprises forming a melt the silicon content of which is materially less than is desired in the casting, add-- ing silicon, and casting the melt substantially immediately after the addition of silicon.
3. Method of producing a ferrous alloy casting having substantially the composition: 0.1% to 2% chromium, 1% to 4% silicon, 1% to 4% carbon, 0.15% to 1% manganese, upto about 0.5% sulfur, up to about 0.3% phosphorus, the remainder iron, and characterized by improved machinability, ductility, and strength, which comprises forming a melt the silicon content of which is materially less than is desired in the casting, adding silicon, and casting the melt substantially immediately after the addition of silicon.
4. Method of producing an alloyed cast-iron casting containing from 0.1% to 15% chromium which comprises forming a melt of chromiumalloyed iron the silicon content of which is materially less than is desired in the casting, adding silicon, and casting the melt substantially immediately after the addition of silicon, whereby is produced a casting having a structure consisting chiefly of a pearlitic ground mass, small graphite flakes, and small widely dispersed non-dendritic carbide particles distributed substantially uniformly throughout the ground mass the proportion of carbide present being only a minor fraction of that normally present in cast iron of similar composition.
CHARLES 0. BURGESS.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US682275A US2038639A (en) | 1933-07-26 | 1933-07-26 | Method of producing castings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US682275A US2038639A (en) | 1933-07-26 | 1933-07-26 | Method of producing castings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2038639A true US2038639A (en) | 1936-04-28 |
Family
ID=24738982
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US682275A Expired - Lifetime US2038639A (en) | 1933-07-26 | 1933-07-26 | Method of producing castings |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2038639A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3035911A (en) * | 1960-07-29 | 1962-05-22 | Harry H Kessler | Cast iron |
| US3432290A (en) * | 1966-05-02 | 1969-03-11 | Brico Eng | Ferrous material |
| US3849078A (en) * | 1972-10-19 | 1974-11-19 | Caterpillar Tractor Co | A sealing ring of stainless iron base alloy |
| US3849122A (en) * | 1972-10-19 | 1974-11-19 | Caterpillar Tractor Co | Stainless iron base alloy metal-to-metal high speed seals |
| US4345943A (en) * | 1979-04-26 | 1982-08-24 | Nippon Piston Ring Co., Ltd. | Abrasion resistant sintered alloy for internal combustion engines |
-
1933
- 1933-07-26 US US682275A patent/US2038639A/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3035911A (en) * | 1960-07-29 | 1962-05-22 | Harry H Kessler | Cast iron |
| US3432290A (en) * | 1966-05-02 | 1969-03-11 | Brico Eng | Ferrous material |
| US3849078A (en) * | 1972-10-19 | 1974-11-19 | Caterpillar Tractor Co | A sealing ring of stainless iron base alloy |
| US3849122A (en) * | 1972-10-19 | 1974-11-19 | Caterpillar Tractor Co | Stainless iron base alloy metal-to-metal high speed seals |
| US4345943A (en) * | 1979-04-26 | 1982-08-24 | Nippon Piston Ring Co., Ltd. | Abrasion resistant sintered alloy for internal combustion engines |
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